N751UW
Service difficulty reports · 250
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N751UW' AND registry_match = 'registration' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N751UW' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR AALA201705129022Ballscrew · damagedNR 1 ENGINE HAS AN ECAM FOR A STALL. MX FOUND THE VBVS STUCK OPEN AND SEVERAL OF THE CABLE`S BIRD CAGED, ALSO THE MASTER AND SLAVE ACTUATORS NEED REPLACED. AIRCRAFT WAS GROUNDED.SDR AALA201705119015Actuator · failedDIVERTED DUE TO LEFT ENGINE SURGE INDICATION. PILOT REPORTED THAT HE FELT AND HEARD AUDIBLE STALL AND THE AIRCRAFT YAWED. NO EMERGENCY DECLARED AND LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND VBVS STUCK IN OPEN POSITION WITH DAMAGED DRIVESDR AALA201704279006Floor Panel · delaminatedAIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON FORWARD CARGO PANEL 131AF. REPLACED FORWARD CARGO PANEL 131AF PER AMM 53-22-14.SDR AALA201610139022Lens · missingL2 DOOR EXIT LENS. INSTALLED LENS COVER AT L2 DOOR. IPC 33-51-13 IAW GPM NO TECH REF SEE TEXT FOR MAINT OR REPAIR DONE. THE AIRCRAFT WAS NOT GROUNDED.SDR AALA201603299009Plate · crackedAIRCRAFT IN BASE MX. RT KEEL BEAM CONNECTING PLATE CRACKED AT FRAME 42 & STRINGER 36 RT. REPLACED CONNECTING PLATE IAW SRM 53-36-11 & DWG D53370682.SDR AALA201603099010Lens · brokenEMERGENCY EXIT LIGHT COVER ROW 3 LT BROKE. INSTALLED EMER EXIT LIGHT LENS AT ROW 3 LT. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-19.SDR AALA201602069003Latch · lack of lubeAIRCRAFT WAS NOT GNDED. 2R DOOR DIFFICULT TO ARM. LUBRICATED LATCHES FOR GIRT BARS & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.SDR AALA201510219006Seat · out of adjustSEAT 8D & E RECLINE INTO EXIT ROW. SECURED SEATS IN THE UPRIGHT POSITION.SDR AALA201506109002Fan · malfunctionedFLIGHT 682 EN-ROUTE THE FLIGHT DIVERTED DUE TO SOME TYPE OF ELEC SMELL DETECTED IN THE CABIN. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. REPLACED THE RT RECIRCULATION FAN.SDR USAA2015030500003Lens · brokenEMERGENCY LIGHT LENS BROKEN AT SEAT 3C. REPLACED LENS ON SEAT 3C. OPERATIONAL CHECKED OK.SDR USAA2015021200002Lens · missingSEAT 10D SEAT MOUNTED EMER EXIT LOCATION LIGHT RED LENS MISSING. REPLACED SEAT MOUNTED EMER EXIT LOCATION LIGHT RED LENS ON SEAT 10D IAW AMM 33-51-18-401. OPERATIONAL CHECKED GOOD.SDR USAA2014123000003Flashlight · inoperativeFORWARD FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. REPLACED FWD FLIGHT ATTENDANT FLASHLIGHT. OPERATIONS CHECKED GOOD.SDR USAA2014100900004Lens · missingTHE EMER LENS COVER MISSING AT SEAT 3C. INSTALLED EMER LENS COVER AT SEAT 3C IAW AMM 33-50-00. OK FOR USE.SDR USAA2014070200003Cover · damagedTHE EMER EXIT LIGHT LENS COVER DAMAGED AT SEAT ROW 1 LT. REPLACED EMER EXIT LIGHT LENS COVER AT SEAT ROW 1 LT. OK FOR SERVICE.SDR USAA2014070100007Megaphone · inoperativeTHE FWD MEGA PHONE INOPERATIVE. REPLACED FWD MEGA PHONE. OK FOR SERVICE.SDR USAA2014061200010Lens · missingTHE EXIT PATH LIGHT AT L1 MISSING COVER. REPLACED LENS ON EMER LIGHT. OPERATIONS CHECKED GOOD.SDR USAA2014051200033Mechanism · unserviceableTHE FWD ENTRY DOOR, DOOR LOCK MECHANISM, REQUIRES REPLACEMENT. R & R L1 DOOR LOCK, STAY, MECHANISM IAW AMM 52-11-12-000-001. OPERATIONS CHECKED GOOD.SDR USAA2014051200006Cylinder · unserviceableTHE L1 DOOR DAMPER DOES NOT DAMPEN DOOR WHEN OPENING. REPLACED DOOR DAMPER & EMERGENCY OPERATION CYLINDER IAW AMM 52-11-14-400-001-B.SDR USAA2014021700005Smoke Detector · faultyCREW REPORTED A SMOKE DETECTOR FAULT. TROUBLE SHOT FOR A DOUBLE CHANNEL FAILURE IAW TSM 26-17-00-810-803-A. FOUND DETECTOR 2WH AT FAULT. R & R DETECTOR 2WH IAW AMM 26-16-15-400-001-A. ACCOMPLISHED SATISFACTORY OPERATIONAL TEST OF CARGO COMPARTMENT SMOKE DESDR USAA2013121200008Control Unit · faultyEN ROUTE FROM IND TO CLT, CREW REPORTED THE CB TRIPPED ON OVERHEAD FOR LT FUEL TANK TRANSFER AT 30,000 FEET. CREW DECLARED AN EMERGENCY TO EXPEDITE THEIR ARRIVAL IN CLT. FLIGHT LANDED WITHOUT INCIDENT. TROUBLESHOT TO NR 1 FLSCU. R & R NR 1 FLSCU IAW AMM 28SDR USAA2013111200008Lens · missingMAINTENANCE REPORTED THE EMERGENCY LIGHT LENS MISSING AT 2 LEFT. MAINTENANCE REPLACED EMERGENCY LIGHT LENS IAW AMM 33-50-00. LIGHT OPS CHECKED OK.SDR USAA2013102800028Fitting · dirtyCREW REPORTED, R2 DOOR VERY DIFFICULT TO DISARM, MAINTENANCE CLEANED DEBRIS FROM R2 DOOR GIRT BAR FITTINGS. SLIDE ARMS AND DISARMS NORMALLY. OK FOR SERVICE.SDR USAA2013072900039Fairing · faultyCREW REPORTED THE WINDOW SHADE IN EMERGENCY EXIT ROW 9F BROKEN, OBSCURES VIEW OF WINDOW WHEN STUCK IN CLOSED POSITION. MX REPLACED WINDOW FAIRING ASSY IAW AMM AND IPC 25-23-47.SDR USAA2013061800008Seat · inoperativeCREW REPORTED THE HORIZONTAL MECHANICAL ADJUSTMENT ON F/O SEAT IN INOP. MX REPLACED F/O'S SEAT IAW AMM 25-11-51-000-001-A. CHECKS NORMAL.SDR USAA2013042900022Proximity Sensor · faultyDURING APPROACH, CREW RECEIVED A LGCIU NR 2 FAULT AND A NR 2 THRUST REVERSER FAULT. ALL THREE LANDING GEAR LIGHTS INDICATED GREEN AND WERE DOWN AND LOCKED. CREW DECLARED AN EMERGENCY AS A PRECAUTION. THE FLIGHT LANDED WITHOUT INCIDENT AND TAXIED TO THE GATSDR USAA2013030500010Lens · missingMAINTENANCE REPORTED THE SEAT MOUNTED EMERGENCY EXIT LIGHT LENS MISSING ON SEATS 1C, 3C AND 10D. MAINTENANCE REPLACED LENSES PER AMM 33-51-19, PB 401.SDR USAA2013010200012Nut Plate · wrong partCREW REPORTED DOOR L2 SLIDE DOES NOT SHOW ARMED IN FLIGHT. MAINTENANCE FOUND THE L2 DOOR GIRT BAR FITTINGS TO BE INSTALLED WITH WRONG PARTS. REMOVED AND REPLACED GIRT BAR FITTING NUT PLATE ASSEMBLIES INTO PROPER POSITIONS. P/N D5348023000200 AND P/N D534802SDR USAA2012123100008Mechanism · obstructedCREW REPORTED THAT DOOR 2L SLIDE DOES NOT INDICATE ARMED WHILE IN FLIGHT. MAINTENANCE CLEANED DEBRIS FROM DOOR AREA AND MECHANISM. OPS CHECK OK.SDR USAA2012122800011Damper · out of tolerance2S CHECK - OUT OF ADJUSTMENT DIMENSION BETWEEN FINGER AND STRIKER LEVER OF DOOR DAMPER MECHANISM & EMERGENCY OPERATION CYLINDER AT DOOR 831. PERFORMED ADJUSTMENT OF DIMENSION A BETWEEN FINGER AND STRIKER LEVER OF DOOR DAMPER MECHANISM & EMERGENCY OPERATION CYSDR USAA2012122800010Damper · out of tolerance2S CHECK - OUT ADJUSTMENT DIMENSION A BETWEEN FINGER AND STRIKER LEVER OF DOOR DAMPER MECHANISM & EMERGENCY OPERATION CYLINDER AT DOOR 832. PERFORMED ADJUSTMENT OF DIMENSION A BETWEEN FINGER AND STRIKER LEVER OF DOOR DAMPER MECHANISM & EMERGENCY OPERATION CYLSDR USAA2012122600012Hinge Fitting · excess play2S CHECK - EXCESSIVE PLAY AT NR 5 RUDDER HINGE BEARING AT STABILIZER STA 299, RIB 4. REPLACED NR 7 RUDDER HINGE ARM FITTING AT STABILIZER STA 299, RIB 7 IAW A319 AMM 55-36-41 & SRM 51-42-11.SDR USAA2012122600011Hinge Fitting · excess play2S CHECK - EXCESSIVE PLAY AT NR 2 RUDDER HINGE BEARING AT STABILIZER STA 193, RIB 4. REPLACED NR 2 RUDDER HINGE ARM FITTING AT STABILIZER STA 193, RIB 4 IAW A319 AMM 55-36-41 & SRM 51-42-11.SDR USAA2012123100019Fuel Door · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION IN COUNTERSINK HOLES OF RIGHT WING FUEL DOOR 640RB BETWEEN RIB 21 TO RIB 22 & BETWEEN S8R TO S11R. REPLACED RIGHT WING FUEL DOOR 640RB IAW A319 AMM 57-27-11-400-002-A.SDR USAA2012121800007Fitting · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON CENTER FITTING BETWEEN FR16 TO FR20, S23L. REPLACED CENTER FITTING BETWEEN FR16 TO FR20, S23L IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53112109.SDR USAA2012123100018Fuel Door · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION IN COUNTERSINK HOLES OF RIGHT WING FUEL DOOR 640LB BETWEEN RIB 16 TO RIB 17 & BETWEEN S8R TO S11R. REPLACED RIGHT WING FUEL DOOR 640LB IAW A319 AMM 57-27-11-400-002-A.SDR USAA2012122800004Fuel Door · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON LOWER LEFT WING FUEL DOOR 540HB BETWEEN WS 7316 TO WS 7792, BETWEEN S8L TO S11L & BETWEEN RIB 13 TO RIB 14. REPLACED LOWER LEFT WING FUEL DOOR 540HB IAW A319 SRM 51-72-11 & 57-27-11 PARA 4B ITEM 4.SDR USAA2012122800003Hinge Fitting · worn2S CHECK - WEAR ON RIGHT WING NR 2 SPOILER CENTER HINGE FITTING BETWEEN WS 613 & WS 670 & BETWEEN RIB 11 & RIB 12. REPAIRED RIGHT WING NR 2 SPOILER CENTER HINGE FITTING IAW A319 SRM A319 57-70-00 PARAG 5C FIG 201.SDR USAA2012121800006Fitting · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON CENTER FITTING BETWEEN FR16 TO FR20, S23R. REPLACED CENTER FITTING BETWEEN FR16 TO FR20, S23R IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53112109.SDR USAA2012123100021Skin Panel · corroded2S CHECK - CORROSION ON PLATE LOCATED ON INTERNAL SKIN PANEL BETWEEN FR63 TO FR64 & BETWEEN S41R TO S42R. REPAIRED INTERNAL SKIN PANEL BETWEEN FR63 TO FR64 & BETWEEN S41R TO S42R IAW EA 503627.SDR USAA2012123100020Skin Panel · corroded2S CHECK - CORROSION ON PLATE LOCATED ON INTERNAL SKIN PANEL BETWEEN FR63 TO FR64 & BETWEEN S41L TO S42L. REPAIRED INTERNAL SKIN PANEL BETWEEN FR63 TO FR64 & BETWEEN S41L TO S42L IAW EA 503615.SDR USAA2012122600010Sill · corroded2S CHECK - CORROSION ON R2 DOOR SILL AT FR68, S23R. REPAIRED R2 DOOR SILL AT FR68, S23R IAW EA 202061.SDR USAA2012123100023Seat Track · corroded2S CHECK - LEVEL 2 EXFOLIATION CORROSION ON SEAT TRACK BETWEEN FR24 TO FR35, -Y1292. REPLACED SEAT TRACK BETWEEN FR24 TO FR35, -Y1292 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53110920.SDR USAA2012121800011Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR36 TO FR41, Y1292. REPLACED SEAT TRACK BETWEEN FR36 TO FR41, Y1292 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53370500.SDR USAA2012121800010Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR36 TO FR41, Y765. REPLACED SEAT TRACK BETWEEN FR36 TO FR41, Y765 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D57130147 & D53370500.SDR USAA2012123100003Angle · cracked2S CHECK - CRACK ON SEGMENT ANGLE ON EMERGENCY EXIT DOOR 844 BETWEEN FR40 TO FR41 & BETWEEN BEAM 1 TO BEAM 3. REPLACED SEGMENT ANGLE ON EMERGENCY EXIT DOOR 844 BETWEEN FR40 TO FR41 & BETWEEN BEAM 1 TO BEAM 3 IAW EO 5210Y228.SDR USAA2012123100002Angle · cracked2S CHECK - CRACK ON SEGMENT ANGLE ON EMERGENCY EXIT DOOR 834 BETWEEN FR40 TO FR41 & BETWEEN BEAM 1 TO BEAM 3. REPLACED SEGMENT ANGLE ON EMERGENCY EXIT DOOR 834 BETWEEN FR40 TO FR41 & BETWEEN BEAM 1 TO BEAM 3 IAW EO 5210Y228.SDR USAA2012122800007Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT RAIL BETWEEN FR46+16 INCHES TO FR47/51, -Y1292. REPLACED SEAT RAIL BETWEEN FR46+16 INCHES TO FR47/51, -Y1292 IAW A319 SRM 57-41-15 PARAGRAPH 5B FIG 202.SDR USAA2012121200008Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 232AH BETWEEN FR28 TO FR35 & BETWEEN -Y1732 TO -Y1292. REPLACED FLOOR PANEL 232AH IAW A319 SRM SUPPLEMENTAL INF. 53-02-00-201 FIG 209 & IRM 9701 REV G.SDR USAA2012122800006Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR20 TO FR23, -Y765. REPLACED SEAT TRACK BETWEEN FR20 TO FR23, -Y765 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53112812.SDR USAA2012123100022Flap · corroded2S CHECK - LEVEL 2 EXFOLIATION CORROSION ON LEFT WING OUTBOARD FLAP AT RIB 14. REPLACED LEFT WING OUTBOARD FLAP IAW A319 AMM 27-54-62-400-001-A.
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